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Tamir Gazit


Last seen: quasi 2 anni fa |  Attivo dal 2020

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Boeing 737-300 - VLM - panel method
Calculation of Cl(y) and Cp(y) using VLM method.

oltre 4 anni fa | 2 download |

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NACA 2412 - vortex divsion over the chord
NACA 2412 pressure on the upper and lower surface.

oltre 4 anni fa | 3 download |

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NACA 00XX - doublet divison over the chord
NACA 00XX - doublet divison over the chord compard to Abbott & Von Doenhoff book.

oltre 4 anni fa | 1 download |

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aeroelastic deformations efficiency - divergence speed
This code computs static aeroelastic deformations and aeroelastic efficiency of a wind-tunnel model at different fflow condition...

oltre 4 anni fa | 5 download |

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